JASC 5410
Service difficulty reports · 4,114
Reports filed under 5410 · Nacelle/Pylon, Main Frame, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5410' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5410' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR WX0A2024050832034Acoustic Panel · dented(DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 4000-0006: LOWER ACOUSTIC PANEL DENTED ON #2 ENG NOSE COWL. / LOWER ACOUSTIC PANEL DENT ON #2 ENG NOSE COWL LOCATED AT 6 O'CLOCK AND 3.550 IN FROM L/E WAS EVALUATED WITHIN REPAIRABLE LIMITS AS PER NSRSDR HYIA20230425001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE OUTBOARD LEG OF THE RIGHT HAND INBOARD NACELLE FITTING, (P/N: 5292029-22) THIS CRACK MEASURES APPROXIMATELY .250 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXSDR R61A2024050600198Rib · crackedRH AFT FIXED PYLON FAIRING FOUND TO HAVE 4 CRACKED RIBS. REMOVED AND REPLACED 3 RIBS AT RH AFT FIXED PYLON FAIRING IAW EMBRAER 175 SRM 51-43-01 AND SRM 51-42-01. 1 RIB WAS REPLACED W LOCAL MAN / MADE REPAIR PART IAW DWG 171-03478-001 AND INSTALLED IAW SRM 1-4SDR SWAA2024052277062Shield · cracked#1 ENGINE I/B FAN COWL OIL DOOR SHEILD HAS A CRACK<[01] REMOVE AND INSTALL NEW SHIELD ON #1 ENINE I/B FAN COWL STRUCTURE IAW SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR SWAA2024052277063Shield · cracked#2 ENGINE O/B FAN COWL OIL DOOR SHEILD HAS A CRACK<[01] REMOVE AND INSTALL NEW SHIELD ON #2 ENINE O/B FAN COWL STRUCTURE IAW SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.SDR IPXA2024042679193Bracket · cracked*** SUPPLEMENTAL SDR *** FAULT - CRACK - BRACKET, NO.1 ENGINE LH AFT LOWER LPT COOLING MANIFOLD DUCT SUPPORT AT 7:30 POS (REPLACE) 1. I.A.W. AMM 75-24-03-004-050-H00 & 75-24-03-404-037-H00, REV: 141, REPLACED THE LPTACC MANIFOLD WITH SERVICEABLE PARTS. 2. COMPSDR CALA2024042201196Fairing · crackedNUMBER 1 PYLON OTBD SIDE TE FAIRING CRACKED AT STRINGER ATTACH POINT. NR 1 PYLON OB SIDE STRINGER ATTACHMENT SPLICE PLATE WAS REMOVED AND REPLACED IAW SRM 51-40-02 PARAGRAPH 7. DRAWING 313T3380, NEW PART 313T3380-659 WAS INSTALLED PER AMES REA 7609REA03 ANDSDR CALA2024042201160Support Rib · crackedRT PYLON AFT LOWER FAIRING TIP INTERNAL SUPPORT RIB CRACKED REF AAR N/R 9882924 REMOVED AND REPLACED NO.2 PYLON T/E FAIRING REF SRM 51-40-02-0G-0 DWG 313A2752 AND 313A2752.SDR DALA2024041504458Blowout Panel · openATB - DUE TO R ENG UPPER PYLON PANEL BLOW OUT PANEL OPEN. CORRECTIVE ACTION: INSTALLED NEW BLOWOUT DOOR, EXPANSION JOINT, DUCT, VENTURI DUCT, AND SEALS. OPS AND LEAK CHECKS GOOD.SDR DALA2024041104321Cowl Door · corrodedSHIP 5648 RH ENGINE INLET COWL LE LIP HAS NUMEROUS AREAS OF LIGHT SURFACE CORROSION AROUND ENTIRE LIP. CORRECTIVE ACTION: C/W ER/A 616770-14 REV ORIGINAL AT RH ENGINE INLET COWL LE LIP. (0286817)SDR UIEA2024032200187Door · chafed#1 ENG RH CORE COWL PRESSURE RELIEF DOOR INTERNAL UPPER FND 1EA FRAME CHAFING(<P>FRAME CHAFING AREA REPAIRED AS PER EO 1971A308 REV 0. NO FURTHER DEFECTS NOTED </P>)SDR UIEA2024032400209Beam · cracked#1 PYLON INBD SKIRT BEAM AFT STRUT ADP AIR OUTLET UPPER FND PYLON PANEL FASTENER HOLES CRACKED (2 LOCATIONS)(<P>SKIN 2EA FASTENER HOLES REPAIRED AS PER RI-54-51-16818 REV A. NO FURTHER DEFECTS NOTED</P>)SDR AALA202404100149Lug · crackedAIRCRAFT WAS NOT GROUNDED: NUMBER 2 ENGINE, NUMBER 1 PLATFORM HAS CRACKED LUG. REMOVE AND REPLACED NUMBER 2 ENGINE PLATFORM SET. PER MCM 4901.SDR SWAA2024041071898Door · inflt separation#2 ENG COWL (BOTH SIDES) DEPARTED A/C SHORTLY AFTER TAKEOFF NO ABNORMAL ENGINE INDICATIONS. NO ABNORMAL FLIGHT CHARACTERISTICS NOTED. COMPLIED WITH CONDITONAL INSPECTION 05-51-59.SDR CALA2024040800992Bolt · missingRH ENG PYLON HYDRAULIC BAY INBD ACCESS PANEL ONE BOLT MISSING FROM LATCH THIRD LATCH BACK HAS UPPER SCREW MISSING FROM LATCH QC 1 CYCLE BUT BEFORE 2 FLIGHT CYCLES PART 1 INTERIM REPAIR ACCOMPLISHED IAW EC/RA 5453-01262.PERMANENT REPAIR TO BE ACCOMPLISHED PER PSDR VNAA202404160010Cowling · dentedRH NACELLE, I/B SIDE, FAN COWL PANEL (442AB), TOP EDGE OF PANEL DAMAGED (2 DENTS) APPROX. 12" FROM AFT END OF PANEL. DAMAGE CLASSIFIED IN PSA AIRLINES EA A1-690-54-00024 REV A.SDR VNAA202404160009Fairing · unserviceableRH ENGINE, FWD FAN COWL HINGE LINE FAIRING DAMAGED/BENT BEYOND REPAIR LIMITS. (PANEL 442BB)SDR 21GA20240403009Stiffener · wornENG NO. 2 LH INBOARD THRUST REVERSER STIFFENER DAMAGEDSDR 21GA20240403008Strut · crackedENG NO. 2 PYLON RH STRUT SIDE AFT TRAPEZOIDAL ACCESS DOOR CRACKED.SDR 21GA20240403007Frame · damagedENG INBD COWLING FRAME DAMAGESDR CALA2024041101042Access Panel · damagedWHILE PERFORMING A WALK AROUND FOUND #2 ENGINE STARTER ACCESS PANEL OPEN UPON ARRIVAL TO THE GATE FROM FLIGHT. TRIED TO CLOSE PANEL WITH NO HELP. PANEL IS UNEVEN AND NOT FLUSH WITH THE ENGINE STRUCTURE. REMOVED AND REPLACED ENG #2 CTR T/R ACCESS PNL. ACCESS PNSDR S9BA20240402001Longeron · crackedRH ENGINE NACELLE OUTBOARD LOWER LONGERON CRACKED.SDR DALA2024040103926Spigot · corrodedSHIP 3139 CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. CORRECTIVE ACTION: REMOVED AND REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER A319 SRM 54-51-12-300-001. (0270062)SDR DALA2024040103931Spigot · corrodedSHIP 3139 CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. CORRECTIVE CTION: REMOVED AND REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001. (0270073)SDR IXXA2025012902Fan Cowl · gougedRUB PLATE GOUGED OUTBD FAN COWL PN 224-2202-507 # 2 ENGINESDR CALA2024040200924Panel · missingNR 1 ENGINE PYLON PANEL HEAT SHIELD COATING MISSING FROM LOWER SECTION OF PANEL - APPROXIMATLY 10 SQ INCHES. REMOVED ENG 1 INBD AFT PYLON ACEESS PANEL FOR MX AT IAH. INSTALLED #1 ENGINE INBOARD PYLON PANEL REF AMM 54-53-01.SDR SWIA2024052000327Door · chafedRH ENG NACELLE TRAN COWL LEADING EDGE OUTBD INTERNAL CHAFING (C-CHECK RO 5/20/2024) PERFORMED REPAIR ON DAMAGE HOLES AT RH UPPER TRAN COWL INNER SKIN AND FORWARD DISHING IAW REO 670-54-21-1632 REV-- DATE: 2024-05-13 AND SRM 51-21-11, SRM 51-25-06, SRM 51-2SDR UIEA2024032400211Access Door · damagedON POST FLT, FOUND #4 ENG INBD PYLON DAMAGED (SAIL BOAT DOOR)(<P>TEMP REPAIR TO #4 ENG PYLON PANEL COMPLETED PEREA 4454A0080 & SRM 51-70-19-0G-0. SCHEDULED PERMANENT REPAIR UPON AIRCRAFT RETURN TO MIA FROM SCL PRIOR TO THE ACCUMULATION OF 2 F/C AFTER TIME LIMISDR DALA2024032503722Fillet · damagedSHIP 3134 DAMAGE TO RT PYLON OUTBOARD FILLET FAIRING 482AR. CORRECTIVE ACTION: REPAIRED PER A319 SRM 54-50-00-300-017. (5520952)SDR CALA2024032500854Panel · crackedGEN ITEM; EA 5720-03041 REV E OP 006/// NO 2 ENGINE PYLON TO WIN G LEADING EDGE PANEL ASSEMBLY CRACKED. PANEL ASSEMBLY IS CURRENT LY REMOVED FROM THE AIRCRAFT. REPORTED BY V932161SDR IXXA2024041403Support Frame · gougedTOP PORTION OF #2 ENGINE STRUT FAIRING SUPPORT STRUCTURE FRAME -136 GOUGEDSDR CALA2024032200832Access Panel · missingPDA, R/H ENGINE STRUT PRESSURE RELIEF DOOR/ACCESS PANEL 443CL FOUND MISSING ON ARRIVAL. PHOTO ADDED. NIL STOCK LHR. CDL APPLIED. CDL APPLIED. SDR RAISED #1035496 DISPATCH DESK: 67 NAME: AC DATE: 19-MAR-24- OK TO PLACE PDA 2 R/H ENGINE STRUT PRESSURE RELIEF DOOSDR SWAA2024041065014Cowling · cracked#2 ENGINE I/B FAN COWL LOWER FWD END CRACK<[01] ACCOMPLISHED REMOVAL; REPLACEMENT AND ADJUSTMENT OF #2 ENGINE I/B FAN COWL AS PER AMM 71-11-02-000-802-F00;71-11-02-400-802-F00 AND 71-11-03-820-001;[02] VERIFIED STEP 1 FINALSDR HALA20240318068Hinge Fitting · damagedWHILE OPENING IMBOARD(RIGHT) FAN COWL DOOR ON ENG 1 FOR ENGINE 1A CHECK, FOUND CRACK ON FAN COWL DOOR. SECONDARY STRUCTURE ON PYLON TO NACELLE STRUCTURE CRACKED 3.5" ON RIVET LINE. RH FAN COWL DOOR SECOND HINGE MOUNTING BOLT NUT/WASHER ASSEMBLY HAS WORN THROUGSDR SWAA2024040364051Web · cracked#1ENG. INBD.COWL;PNL. 414; WEB SUPPORT ATTACHMENT AT OIL SERV. DOOR OPENING CRACKED.<[01] REMOVED AND REPLACED WEB PER CMM 71-13-30.;[02] INSPECTED CA #1SDR CALA2024031800748Attach Angle · crackedREMOVED AND REPLACED #2 PYLON IB AFT FAIRING ATTACHED ANGLE IAW B767-300 SRM 51-40-02 PARA 7SDR FDEA202403150292Fairing · damaged#3 ENGINE PYLON AFT FAIRINGS DAMAGED. AMM: 54-81-01-4 INSTALLED SERVICEABLE PYLON FAIRINGSDR SWAA2024041768553Seal · debondedPANEL 433BT PANEL ASSEMBLY - UPPER SPAR WEB - #1 ENGINE HAS DISBONDED RUBBER SEAL.<[01] REPLACED PANEL; PANEL TO BE INSTALLED ON CLOSE TASK CARD TTG8Q00R9FRX (#960)SDR DALA2024031303310Drag Fitting · damagedSHIP 6821 AD - SCRATCHES ON LH ENG DRAG FTG HOLES AS FOLLOW: HOLE #12 SCRATCHES ON SKIN & FTG BTW 3 TO 6 O CLOCK POSITION, HOLE #13 SCRATCHES ON SKIN & FTG BTW 9 TO 12 AND 3 TO 6 O CLOCK POSITION AND HOLE #16 SCRATCHES ON SKIN & FTG ALL AROUND. (IN REFERENCE TSDR DALA2024031303309Drag Fitting · damagedSHIP 6821 AD - SCRATCHES ON LH ENG DRAG FTG HOLES AS FOLLOW: HOLE #2 ON SKIN & FTG BTW 3 TO 6 O CLOCK POSITION, HOLE #5 ON SKIN BTW 6 TO 9 O CLOCK POSITION, HOLE #8 ON SKIN & FTG BTW 9 TO 12 O CLOCK POSITION (IN REFERENCE TO JOB 114-0001 CARD). CORRECTIVE ACTISDR YENA2024031200401Plate · corrodedDURING HEAVY MAINTENANCE: RETAINING PLATE WAS FOUND WITH CORROSION ON R/H SPIGOT; REMOVED AND REPLACED LOWER SILL LOC. BTW FR60 TO FR62 AT LEVEL STR38R IAW A320 SRM 53-41-49-300-002. AND DWG E534770321. THIS REPAIR IS CATEGORY A. NO REQUIRED FURTHER INSPECTIONSDR YENA2024031200390Spar · unknownDURING HEAVY MAINTENANCE: IN REF NRC 00365:REPLACE INBD UPPER SPAR AT RH PYLON; (RESOLVED ON W/O: 1288392 TASKCARD: NR-00039) REF TOMEX WO 8619, NRC 00394, INBD UPPER SPAR AT RH PYLON WAS REPLACED PER EMB--190 S.R.M. 51-43-03, S.R.M. 51-43-04.SDR AALA202403126562Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON INBOARD SIDE FAN COWL FORWARD HINGE FITTING ON PYLON WORN AT PYLON RIB 1. REPLACED HINGE FITTING PER SRM 51-42-11.SDR AALA202403126881Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON INBOARD SIDE FAN COWL CENTER HINGE FITTING ON PYLON WORN AT PYLON RIB 5. REPLACED HINGE FITTING PER SRM 51-42-11.SDR COEA2024031209734Longeron · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS DISCOVERED ON THE L/H ENGINE LONGERON UNDER THE PLENUM PANEL (LOWER AREA). REPAIR ACCOMPLISHED PER MANUFACTURER AVIATION SERVICES ICT WO 206698 DATED 4/22/2024.SDR JR2R20240307411Fitting · chafedRH PYLON OB WING MAIN BOX FITTING CHAFED ON FLANGE.SDR JR2R20240307387Retainer · chafed#1 LH AFT CORE COWL LOWER REAR SEAL FOUND SEAL RETAINER DAMAGED.SDR YENA2024030500323Spigot · corrodedDURING HEAVY MAINTENANCE: CORROSION ON UPPER SPAR SPIGOT RECEPTACLE ON RH PYLON; REMOVED AND REPLACED SPIGOT LOWER FITTING IAW A320 SRM 54-51-12-283-002, A320 SRM 54-51-12-300-002, AND AMM 54-51-41-400-001-A TOOL USED: CALIPER: P/N: 500-197-30 S/N: A21043111, SDR YENA2024030500322Spigot · corrodedDURING HEAVY MAINTENANCE: CORROSION ON UPPER SPAR SPIGOT RECEPTACLE ON LH PYLON; REMOVED AND REPLACED SPIGOT LOWER FITTING ON LH PYLON IAW A320 SRM 54-51-12-283-002 AND A320 SRM 54-51-12-300-002. TOOL USED: DIGITAL CALIPER P/N: 500-197-30, S/N: A21043111, DUE SDR COEA2024030507734Panel · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE DISCOVERED ON THE L/H ENGINE INBOARD PLENUM PANEL AFT SIDE BY THE UPPER MIDDLE STIFFENER. THIS IS THE SUPPLEMENTAL SDR FOR CORRECTIVE ACTION: WO 256404 NR 22, L/H ENGINE INBOARD PLENUM PANEL WAS REPLACED I
Back to JASC 5410